JP2014159613A5 - - Google Patents

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Publication number
JP2014159613A5
JP2014159613A5 JP2013030404A JP2013030404A JP2014159613A5 JP 2014159613 A5 JP2014159613 A5 JP 2014159613A5 JP 2013030404 A JP2013030404 A JP 2013030404A JP 2013030404 A JP2013030404 A JP 2013030404A JP 2014159613 A5 JP2014159613 A5 JP 2014159613A5
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JP
Japan
Prior art keywords
layer
forming
film
inner cylinder
film formation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2013030404A
Other languages
Japanese (ja)
Other versions
JP6066760B2 (en
JP2014159613A (en
Filing date
Publication date
Application filed filed Critical
Priority to JP2013030404A priority Critical patent/JP6066760B2/en
Priority claimed from JP2013030404A external-priority patent/JP6066760B2/en
Priority to US14/764,766 priority patent/US9951426B2/en
Priority to PCT/JP2013/063896 priority patent/WO2014128983A1/en
Publication of JP2014159613A publication Critical patent/JP2014159613A/en
Publication of JP2014159613A5 publication Critical patent/JP2014159613A5/ja
Application granted granted Critical
Publication of JP6066760B2 publication Critical patent/JP6066760B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Claims (6)

ロケットエンジンの燃焼室の製造方法であって、
前記燃焼室は、同心円状に配置された内筒と外筒とを備え、
前記内筒と前記外筒との間には冷却流路が形成されており、
前記外筒は、
前記内筒側に形成された第1層と、
前記第1層の外側の表面に形成された第2層と
を備え、
前記製造方法は、
前記内筒の表面に複数の溝を形成する工程と、
前記複数の溝に充填材を充填する工程と、
前記充填材及び前記内筒の露出面に導電層を形成する工程と、
前記導電層上に、電鋳法により、第1層を形成する工程と、
前記第1層上に、第2層を形成する工程と
を備え、
前記第2層を形成する工程は、
前記第1層に形成される膜の厚さが所望の膜厚になるまで、単位成膜処理を繰り返し実行するステップを有し、
前記単位成膜処理は、
前記被成膜対象をヒータで熱しながら、コールドスプレー法により前記被成膜対象に対して成膜を行うステップと、
前記成膜後の前記被成膜対象に対して熱処理を施すステップと
を含む
成膜方法。
A method for manufacturing a combustion chamber of a rocket engine,
The combustion chamber includes an inner cylinder and an outer cylinder arranged concentrically,
A cooling flow path is formed between the inner cylinder and the outer cylinder,
The outer cylinder is
A first layer formed on the inner cylinder side;
A second layer formed on an outer surface of the first layer;
With
The manufacturing method includes:
Forming a plurality of grooves on the surface of the inner cylinder;
Filling the plurality of grooves with a filler;
Forming a conductive layer on the exposed surface of the filler and the inner cylinder;
Forming a first layer on the conductive layer by electroforming;
Forming a second layer on the first layer;
With
The step of forming the second layer includes
Repeating the unit film forming process until the thickness of the film formed in the first layer reaches a desired film thickness;
The unit film forming process includes
Performing film formation on the film formation target by a cold spray method while heating the film formation target with a heater;
Applying a heat treatment to the film formation target after the film formation.
請求項1に記載の成膜方法であって、
前記コールドスプレー法により金属膜の成膜が行われる
成膜方法。
The film forming method according to claim 1,
A film forming method in which a metal film is formed by the cold spray method.
請求項1又は2に記載の成膜方法であって、
前記所望の膜厚は1mm以上である
成膜方法。
The film forming method according to claim 1 or 2,
The desired film thickness is 1 mm or more.
請求項1又は2に記載の成膜方法であって、
前記所望の膜厚は10mm以上である
成膜方法。
The film forming method according to claim 1 or 2,
The desired film thickness is 10 mm or more.
ロケットエンジンの燃焼室の製造方法であって、
前記燃焼室は、同心円状に配置された内筒と外筒とを備え、
前記内筒と前記外筒との間には冷却流路が形成されており、
前記外筒は、
前記内筒側に形成された第1層と、
前記第1層の外側の表面に形成された第2層と
を備え、
前記製造方法は、
前記内筒の表面に複数の溝を形成する工程と、
前記複数の溝に充填材を充填する工程と、
前記充填材及び前記内筒の露出面に導電層を形成する工程と、
前記導電層上に、電鋳法により、第1層を形成する工程と、
前記第1層上に、第2層を形成する工程と
を備え、
前記第2層を形成する工程は、
前記内筒をヒータで熱しながら、コールドスプレー法により前記第1層に対して成膜を行い、前記第1層上に膜厚1mm以上の膜を形成するステップを含む
成膜方法。
A method for manufacturing a combustion chamber of a rocket engine,
The combustion chamber includes an inner cylinder and an outer cylinder arranged concentrically,
A cooling flow path is formed between the inner cylinder and the outer cylinder,
The outer cylinder is
A first layer formed on the inner cylinder side;
A second layer formed on an outer surface of the first layer;
With
The manufacturing method includes:
Forming a plurality of grooves on the surface of the inner cylinder;
Filling the plurality of grooves with a filler;
Forming a conductive layer on the exposed surface of the filler and the inner cylinder;
Forming a first layer on the conductive layer by electroforming;
Forming a second layer on the first layer;
With
The step of forming the second layer includes
While heating said inner tube by a heater, subjected to film formation with respect to the first layer by cold spray method, a deposition method comprising the steps of forming a film thickness 1mm or more films on the first layer.
請求項5に記載の成膜方法であって、
前記コールドスプレー法により金属膜の成膜が行われる
成膜方法。
The film forming method according to claim 5,
A film forming method in which a metal film is formed by the cold spray method.
JP2013030404A 2013-02-19 2013-02-19 Deposition method Active JP6066760B2 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP2013030404A JP6066760B2 (en) 2013-02-19 2013-02-19 Deposition method
US14/764,766 US9951426B2 (en) 2013-02-19 2013-05-20 Method for depositing layer
PCT/JP2013/063896 WO2014128983A1 (en) 2013-02-19 2013-05-20 Film forming method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013030404A JP6066760B2 (en) 2013-02-19 2013-02-19 Deposition method

Publications (3)

Publication Number Publication Date
JP2014159613A JP2014159613A (en) 2014-09-04
JP2014159613A5 true JP2014159613A5 (en) 2015-12-17
JP6066760B2 JP6066760B2 (en) 2017-01-25

Family

ID=51390802

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013030404A Active JP6066760B2 (en) 2013-02-19 2013-02-19 Deposition method

Country Status (3)

Country Link
US (1) US9951426B2 (en)
JP (1) JP6066760B2 (en)
WO (1) WO2014128983A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021080943A1 (en) * 2019-10-21 2021-04-29 Westinghouse Electric Company Llc Multiple nozzle design in a cold spray system and associated method

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060121187A1 (en) * 2004-12-03 2006-06-08 Haynes Jeffrey D Vacuum cold spray process
US20060269685A1 (en) * 2005-05-31 2006-11-30 Honeywell International, Inc. Method for coating turbine engine components with high velocity particles
JP2008127676A (en) * 2006-11-24 2008-06-05 Toyohashi Univ Of Technology Formation method of metallic film
JP2009191349A (en) * 2008-02-18 2009-08-27 Honda Motor Co Ltd Method for reforming joining boundary of strengthened film
JP5017675B2 (en) 2008-04-01 2012-09-05 富士岐工産株式会社 Film manufacturing method
JP2010047825A (en) 2008-08-25 2010-03-04 Mitsubishi Heavy Ind Ltd Metal film forming method and aerospace structural member
US20100170937A1 (en) 2009-01-07 2010-07-08 General Electric Company System and Method of Joining Metallic Parts Using Cold Spray Technique
JP5642461B2 (en) * 2010-09-07 2014-12-17 三菱重工業株式会社 Combustion chamber of rocket engine and method for manufacturing hollow structure

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